7150-T61511 Extrusion: MIL-HDBK-5J Design Allowables
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| Material class | Aluminum |
| Alloy / temper / form | 7150 / T61511 / Extrusion |
| Specifications | AMS 4307 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.7.7.0, Table 3.7.7.0(c) (pdf page 430 of the chapter file) |
| Dimension bands | 5 |
| Density | 2823 kg/m³ |
Design Mechanical and Physical Properties (room temperature)
Converted from the handbook table (ksi, Msi, lb/in³) and rounded to 4 significant figures; dimension bands in inches with mm in parentheses. Bases: A and B are statistical minimums (99 % and 90 % probability at 95 % confidence), S the specification minimum. Grain directions: L longitudinal, LT long transverse, ST short transverse.
| Dimension band | 0.250–0.499 in (6.35–12.67 mm) | 0.500–0.749 in (12.7–19.02 mm) | 0.750–0.999 in (19.05–25.37 mm) | 1.000–1.499 in (25.4–38.07 mm) | 1.500–2.000 in (38.1–50.8 mm) | ||
|---|---|---|---|---|---|---|---|
| Specification | AMS 4307 | AMS 4307 | AMS 4307 | AMS 4307 | AMS 4307 | ||
| Basis | S | S | S | A | B | S | |
| Ftu, MPa | L | 599.8 | 606.7 | 613.6 | 613.6 | 648.1 | 613.6 |
| LT | 551.6 | 544.7 | 544.7 | 586.1 | 592.9 | 510.2 | |
| Fty, MPa | L | 565.4 | 572.3 | 579.2 | 572.3 | 606.7 | 579.2 |
| LT | 503.3 | 503.3 | 503.3 | 530.9 | 537.8 | 468.8 | |
| Fcy, MPa | L | 551.6 | 558.5 | 565.4 | 565.4 | 599.8 | 579.2 |
| LT | 551.6 | 551.6 | 551.6 | 530.9 | 558.5 | 517.1 | |
| Fsu, MPa | L | 303.4 | 310.3 | 310.3 | 303.4 | 317.2 | 289.6 |
| LT | 303.4 | 310.3 | 310.3 | 303.4 | 317.2 | 289.6 | |
| Fbru (e/D = 1.5), MPa | L | 820.5 | 827.4 | 827.4 | 813.6 | 861.8 | 799.8 |
| LT | 820.5 | 827.4 | 827.4 | 813.6 | 861.8 | 799.8 | |
| Fbru (e/D = 2.0), MPa | L | 1048 | 1055 | 1062 | 1048 | 1110 | 1034 |
| LT | 1048 | 1055 | 1062 | 1048 | 1110 | 1034 | |
| Fbry (e/D = 1.5), MPa | L | 689.5 | 689.5 | 689.5 | 661.9 | 703.3 | 648.1 |
| LT | 689.5 | 689.5 | 689.5 | 661.9 | 703.3 | 648.1 | |
| Fbry (e/D = 2.0), MPa | L | 813.6 | 827.4 | 827.4 | 806.7 | 854.9 | 806.7 |
| LT | 813.6 | 827.4 | 827.4 | 806.7 | 854.9 | 806.7 | |
| e, % | L | 8 | 9 | 8 | 8 | 8 | 8 |
| LT | … | … | … | … | … | … | |
| E, GPa | 71.71 | 71.71 | 71.71 | 71.71 | 71.71 | 71.71 | |
| Ec, GPa | 75.84 | 75.84 | 75.84 | 75.84 | 75.84 | 75.84 | |
| G, GPa | 27.58 | 27.58 | 27.58 | 27.58 | 27.58 | 27.58 | |
| ν | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | |
| ρ, kg/m³ | 2823 | 2823 | 2823 | 2823 | 2823 | 2823 | |
Effect of Temperature
The handbook maps no temperature-effect figure to this table.
Other 7150 Tables
- 7150-T6151 Plate (Table 3.7.7.0(b))
- 7150-T7751 Plate (Table 3.7.7.0(b))
- 7150-T77511 Extrusion (Table 3.7.7.0(c))
Source and Use
U.S. Department of Defense (2003). Metallic Materials and Elements for Aerospace Vehicle Structures. MIL-HDBK-5J, 31 January 2003 (public domain). The values are the handbook's design allowables as extracted from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ. No warranty is given.